H-3 R/B, 61734

Orbit data source: Space-Track

H-3 R/B, 61734 is space debris originally from a launch on Mon, 04 Nov 2024 UTC launched from the Tanegashima Space Center (TNSTA). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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H-3 R/B details

Identifier	61734, 2024-198B
Orbit	Molniya
Last TLE update	1 day ago
Origin	MHI (JP / JPN)
Manufacturer	MHI Tobishima
Mission	Spacecraft
Bus & Motor	H-2A STAGE 2, Unknown motor
Mass	2,500 kg wet, 2,500 kg dry
Launch date (UTC)	2024-11-04 (1 month ago)
Launch vehicle	Unknown
Launch site	Tanegashima Space Center (TNSTA)
Object type	Payload Rocket body Debris
Shape & HBR	Unknown
Radar Cross Section	RCS unknown

Expand to show TLE details & history

TLE from 1 day ago

0 H-3 R/B
1 61734U 24198B   24347.91942428  .00073230 -72756-6  74058-3 0  9990
2 61734  24.4358 171.8664 7232467 205.5843  85.3640  2.39634819   900

Epoch: 2024-12-12T22:03Z

Definitive object data (Epoch: 2024-12-12T22:03:58.257Z)

Latitude	-0.00029°
Longitude	118.72211°
Altitude	25,935.303 km
Speed	2.788 km/s
True Right ascension	11h 27m 13s
True Declination	0° 00' 01"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	13.32198°
Longitude	149.81099°
Altitude	33,341.128 km
Speed	1.78 km/s
Apparent Right ascension	13h 03m 37s
Apparent Declination	7° 16' 26"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	20:08:36
Azimuth	286.117° WNW
Elevation	-7.562°
Doppler factor	1

Orbital elements

Apogee altitude	34,278.102 km
Perigee altitude	151.252 km
Semi-major axis	23,592.814 km
Eccentricity	0.7232467
Inclination	24.4358°
RAAN	171.8664°
Arg. of periapsis	205.5843°
True anomaly	154.40778°
Mean anomaly	85.364°
Eccentric anomaly	120.91556°
Mean motion	0.59893 °/min
BSTAR	0.00074058
Orbital period	601.08 mins